DAR 6
Design and development
The DAR 6 was designed by Zevtan Lazarov. It was constructed by the Bulgarian State Aircraft Workshops (DAR) .
The aircraft was a conventional biplane with a fixed tailskid landing gear . It was powered by a radial engine .
Three versions were initially developed:
Basic training version, powered by an 85 hp (63 kW) Walter Vega engine;
Advanced training version, powered by a 145 hp (108 kW) Walter Mars I engine;
1937 Model DAR 6a . This variant offered faired struts and redesigned divided landing gear. It was powered by a 150 hp (112 kW) Walter Mars I engine.
Specifications (DAR 6)
Data from The Illustrated Encyclopedia of Aircraft , (Part Work 1982–1985), Orbis Publishing, Page 1295
General characteristics
Crew: two, pilot and student
Length: 6.85 m (22 ft 5.75 in)
Wingspan: 9.05 m (29 ft 8.25 in)
Height: 2.85 m (9 ft 4.25 in)
Wing area: 19.30 m2 (207.75 sq ft)
Empty weight: 510 kg (1,124 lb)
Gross weight: 770 kg (1,697 lb)
Powerplant: 1 × Walter Mars I radial piston engine , 108 kW (145 hp)
Performance
Maximum speed: 180 km/h (112 mph, 97 kn)
Range: 715 km (444 mi, 386 nmi)
References
Wikimedia Commons has media related to
DAR 6 .
Bibliography
Bernád, Dénes (July–August 2001). "Balkan Birds: Thirty-Five Years of Bulgarian Aircraft Production, Part One". Air Enthusiast (94): 18– 30. ISSN 0143-5450 .
The Illustrated Encyclopedia of Aircraft , (Part Work 1982–1985), Orbis Publishing, Page 1295